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Phenom 300 Initial > Limitations (non-red) > Flashcards

Limitations (non-red) Flashcards

1
Q

45 minute IFR reserve fuel

A

1121 Lb

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2
Q

Hot spare fuel

A

3600 Lb

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3
Q

Emergency fuel

A

759 Lb

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4
Q

Inclement Wx fuel

A

3600 Lb

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5
Q

Minimum runway length

A

3500’

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6
Q

Minimum runway width

A

60’

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7
Q

Maximum runway slope

A

+/- 2%

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8
Q

Contaminated runway requires ops review if less than _____

A

5500’

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9
Q

The following equipment must be operational for flight in RVSM airspace

A

Autopilot
AAD
Transponder
ADC X2
Pitot heat X2 on the probes linked to the ADC in use

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10
Q

Zero fuel weight Phenom 300/300E

A

14,220 lb / 14,263 lb

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11
Q

Forward baggage compartment weight limit

A

110 Lb

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12
Q

Aft baggage compartment weight limit

A

463 Lb

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13
Q

Max flaps extended altitude

A

18,000’ MSL

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14
Q

Max OEI altitude in icing

A

15,000’ MSL

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15
Q

Max start/takeoff/landing altitude

A

14,000’ MSL

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16
Q

Max takeoff and landing altitude in icing

A

10,000’ MSL

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17
Q

Minimum start/takeoff/landing altitude

A

-1000’ MSL

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18
Q

Vmo

A

320 Kt

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19
Q

MMO (300/300E)

A

.78/.80

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20
Q

Vmc - Takeoff

A

97/95

21
Q

Vmc - Landing

A

91 Kts

22
Q

Max differential pressure

A

9.4 PSI

23
Q

Max differential overpressure

A

9.6 PSI

24
Q

Maximum differential negative

A

-0.3 PSI

25
Q

Maximum generator load in flight

A

390 A

26
Q

Maximum generator load on ground

A

330 A

27
Q

Battery temperature limit starting without a GPU

A

-18C

28
Q

Maximum fuel 300/300E

A

5401 Lb
5427.6 Lb

29
Q

Maximum fuel imbalance

A

220 Lb

30
Q

Icing conditions exist when:

A

OAT is 10C or below
AND
Visible moisture (rain,snow,vis<1NM)
OR
Operating on contaminated surfaces

31
Q

Minimum temperature - landing

A

-38C

32
Q

Automated operating envelope limit for wing stab heating below 16,000’

A

-40C

33
Q

Automated operating envelope limit for wing stab heating above 16,000’

A

-45C

34
Q

Anti-ice configurations If SAT/TAT is between 5C -10C

A

WSHLD 1&2 - OFF
ENG 1&2 - ON
WING STAB -OFF

35
Q

Anti-ice configurations If SAT/TAT is below 5C

A

WSHLD 1&2 - ON
ENG 1&2 - ON
WING STAB -ON

36
Q

Do not use autopilot if one of the following icing conditions occur:

A

-Ice accumulation on wing aft of the protected area
-Unusual lateral trim inputs or autopilot trim warnings are encountered

37
Q

In case of RTO allow brake cooling time of ____ before subsequent takeoff

A

20 minutes

38
Q

Straight in Vref at max landing weight with swps ice speed EICAS message dispayed is____

A

126 Kt

39
Q

N1 limit for all operating conditions except transient

A

100%

40
Q

N2 limit for all operating conditions except transient, ground idle, and flight idle.

A

101%

41
Q

N2 limit ground idle

A

51.2%

42
Q

N2 limit flight idle

A

55.1%

43
Q

Max ITT at max thrust

A

725C

44
Q

Max ITT at takeoff thrust

A

700C

45
Q

Max ITT at maximum continuous thrust and climb thrust.

A

680C

46
Q

Max ITT starting

A

765C for 5 seconds.

47
Q

Maximum oil consumption

A

1 Qt per 8 hours

48
Q

Minimum oil temp for starting

A

-40C

Phenom 300 Initial (16 decks)

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